This paper describes a piloted simulation conducted on the NASA Ames Vertical Motion Simulator. The objective of the experiment was to investigate the handling qualities benefits attainable using new display law design methods for hover displays. The new display laws provide improved methods to specify the behavior of the display symbol that predicts the vehicle's ground velocity in the horizontal plane; it is the primary symbol that the pilot uses to control aircraft horizontal position. The display law design was applied to the Apache helmet-mounted display format, using the Apache vehicle dynamics to tailor the dynamics of the velocity predictor symbol. The representations of the Apache vehicle used in the display design process and in t...
The study of a control system for the Da Vinci 2 human-powered helicopter in hovering flight is docu...
A dynamic helicopter model was incorporated into an optimal control problem to determine minimal lan...
Early experience in fixed-cockpit simulators, with limited field of view, demonstrated the basic dif...
A simulator evaluation of a cockpit display format for hovering flight is described. The display for...
An analytical and experimental study of the human pilot control strategies in a manned rotorcraft si...
Abstract display as the pilot's only source of outside visual cues. A parallel effort was condu...
Data from a preliminary experiment are presented which attempted to define a helicopter hover task t...
Head-down hover displays and instrument panels theoretically provide all necessary 2ight data inform...
A piloted simulation experiment was conducted using the NASA Ames Research Center Vertical Motion Si...
A mathematical model of an advanced helicopter is described. The model is suitable for use in contro...
To determine motion fidelity requirements, a series of piloted simulations was performed. Several ke...
A piloted simulation experiment conducted on the NASA-Ames Vertical Motion Simulator evaluated the h...
Two computer generated display formats were evaluated as primary displays by six research pilots in ...
A computer aiding concept for low-altitude helicopter flight was developed and evaluated in a real-t...
This paper aims to reveal the effect of different display design principles in the helicopter domain...
The study of a control system for the Da Vinci 2 human-powered helicopter in hovering flight is docu...
A dynamic helicopter model was incorporated into an optimal control problem to determine minimal lan...
Early experience in fixed-cockpit simulators, with limited field of view, demonstrated the basic dif...
A simulator evaluation of a cockpit display format for hovering flight is described. The display for...
An analytical and experimental study of the human pilot control strategies in a manned rotorcraft si...
Abstract display as the pilot's only source of outside visual cues. A parallel effort was condu...
Data from a preliminary experiment are presented which attempted to define a helicopter hover task t...
Head-down hover displays and instrument panels theoretically provide all necessary 2ight data inform...
A piloted simulation experiment was conducted using the NASA Ames Research Center Vertical Motion Si...
A mathematical model of an advanced helicopter is described. The model is suitable for use in contro...
To determine motion fidelity requirements, a series of piloted simulations was performed. Several ke...
A piloted simulation experiment conducted on the NASA-Ames Vertical Motion Simulator evaluated the h...
Two computer generated display formats were evaluated as primary displays by six research pilots in ...
A computer aiding concept for low-altitude helicopter flight was developed and evaluated in a real-t...
This paper aims to reveal the effect of different display design principles in the helicopter domain...
The study of a control system for the Da Vinci 2 human-powered helicopter in hovering flight is docu...
A dynamic helicopter model was incorporated into an optimal control problem to determine minimal lan...
Early experience in fixed-cockpit simulators, with limited field of view, demonstrated the basic dif...